Patents by Inventor Charlotte Dietrich

Charlotte Dietrich has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 10753766
    Abstract: This method for managing the display of a flight profile of an aircraft is implemented by an electronic management device. It comprises computing a reference altitude for the display of a vertical flight profile; determining a range of altitudes for the display of said vertical profile, the range of altitudes being determined as a function of the computed reference altitude, the reference altitude being computed as a function of a current altitude, an altitude interval to be displayed and at least one property relative to an estimated evolution of the altitude of the aircraft from said current altitude.
    Type: Grant
    Filed: February 26, 2019
    Date of Patent: August 25, 2020
    Assignee: THALES
    Inventors: Patrick Cazaux, Sarah Dupont, Charlotte Dietrich
  • Publication number: 20190376812
    Abstract: This method for managing the display of a flight profile of an aircraft is implemented by an electronic management device. It comprises determining a current range of altitudes displayed during the display of a vertical flight profile; and acquiring at least one constraint associated with an upcoming point of a flight plan, each constraint including at least one reference altitude. The method further comprises, when a respective reference altitude is not included in the current displayed altitude range, displaying a symbol representative of the constraint for said reference altitude not included in the current displayed altitude range.
    Type: Application
    Filed: June 6, 2019
    Publication date: December 12, 2019
    Inventors: Patrick CAZAUX, Charlotte DIETRICH, Geoffrey NICOLLET
  • Publication number: 20190277654
    Abstract: This method for managing the display of a flight profile of an aircraft is implemented by an electronic management device. It comprises computing a reference altitude for the display of a vertical flight profile; determining a range of altitudes for the display of said vertical profile, the range of altitudes being determined as a function of the computed reference altitude, the reference altitude being computed as a function of a current altitude, an altitude interval to be displayed and at least one property relative to an estimated evolution of the altitude of the aircraft from said current altitude.
    Type: Application
    Filed: February 26, 2019
    Publication date: September 12, 2019
    Inventors: Patrick CAZAUX, Sarah Dupont, Charlotte Dietrich